Effect of simultaneous cyclic variation of stress and temperature on a high temperature material

  • A. Fransson
Conference paper
Part of the IUTAM Symposia book series (IUTAM)


For the purpose of showing experimentally, by laboratory tests, if a certain high temperature material is suitable for turbine blades in gas turbine engines, it has so far been customary to adopt creep tests and also, occasionally, fatigue tests at high temperatures. Thus, Toolin and Mochel [1], for example, have carried out extensive bending fatigue tests on a great number of high temperature alloys at 1,200 and 1,500° F (650 and 815° C).


Fatigue Titanium Nickel Glycerine Chromium 


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  1. [1]
    Toolin, R. R. and N. L. Mochel: Proc. ASTM 47, 677–694 (1947).Google Scholar
  2. [2]
    Lazan, B. J.: Proc. ASTM 49, 757–787 (1949).Google Scholar
  3. [3]
    Guarnieri, G. J. and L. A. Yerkovich: Proc. ASTM 52, 934–950 (1952).Google Scholar
  4. [4]
    Hignett, H. W. G.: High Temperature Alloys in British Jet Engines. Presented at the meeting of the Detroit Chapter of Amer. Soc. Metals, Nov. 1951.Google Scholar
  5. [5]
    Nordhelm, R. and N. J. Grant: Aging Characteristics of Mckel-Chromium Alloys Hardened with Titanium and Aluminium, Mass. Inst. Tech., 1952.Google Scholar
  6. [6]
    Taylor, A. and R. W. Floyd: J. Inst. Metals 82, 451–464 (1952–53).Google Scholar
  7. [7]
    Floyd, R. W.: J. Inst. Metals 80, 551–553 (1951–52).Google Scholar

Copyright information

© Springer-Verlag OHG., Berlin · Gottingen · Heidelberg 1956

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  • A. Fransson

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